89000109-002
xVue Touch Installation Manual
Rev 2
Page 8-19
© Honeywell International Inc. Do not copy without express permission of Honeywell.
For Use in Non-Certified Aircraft
HDG ALIGNING
The heading source is aligning
• Use the magnetic compass and
the GPS track information for
heading information until the
condition is no longer displayed
• During alignment maintain
wings level (limit airplane to ±5°
in roll and ±5° in pitch) and
maintain constant heading and
airspeed for 3 minutes or until
the alert clears
A/P NAV INOP
Failure of one or more of the four
lateral or vertical deviation
outputs from the KSD 100EXP
Do not use the autopilot NAV or
APPR mode
SVS FAIL
SVS POS Fault:
• If any of the following inputs
become invalid:
o Pitch/Roll Angle
o Body Acceleration (Normal/
Lateral/Longitudinal)
See “Attitude Fail”
troubleshooting procedure in
Table 8-1 xVue Touch System
Troubleshooting Chart
SVS POS Fault:
• If any of the following inputs
become invalid:
o Pressure Altitude
o True Airspeed
o Calibrated Airspeed
See “Altimeter, Airspeed Failures”
troubleshooting procedure in
Table 8-1 xVue Touch System
Troubleshooting Chart
SVS POS Fault:
• If any of the following inputs
become invalid:
o Magnetic Heading
See “Heading Fail”
troubleshooting procedure in
Table 8-1 xVue Touch System
Troubleshooting Chart
SVS POS Fault:
• If any of the following inputs
become invalid:
o Geometric Altitude
o Latitude/Longitude
o Ground Speed
o Magnetic Variation
o True Track
See “No Navigation Data or
Failure” troubleshooting
procedure in Table 8-1 xVue Touch
System Troubleshooting Chart
SVS TER Fault:
• Failure To Receive Terrain Data
From the Terrain Server
• Internal Terrain Rendering Error
Check that airplane maneuvers
are within boundaries of the high
resolution database
Table 8-6 Alerts Troubleshooting Chart
Symptom
Causes
Corrective Action
